Investigation into skin stiffener debonding of top-hat stiffened composite structures

Author:

Yetman J.E.,Sobey A.J.,Blake J.I.R.,Shenoi R.A.

Funder

EPSRC

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference24 articles.

1. Failure of thick-skinned stiffener runout sections loaded in uniaxial compression;Falzon;Compos Struct,2001

2. Stiffener debonding mechanisms in post-buckled CFRP aerospace panels;Meeks;Compos Part A: Appl Sci Manuf,2005

3. The analysis of skin-to-stiffener debonding in composite aerospace structures;Yap;Compos Struct,2002

4. Influence of post-buckling behaviour of composite stiffened panels on the damage criticality;Yap;Compos Struct,2004

5. Wiggenraad J, Greenhalg E, Olsson R, Design and analysis of stiffened composite panels for damage resistance and tolerance, in: 5th world congress on computational mechanics. WCCM V, Vienna; 2002, Vienna University of Technology, 1–493, , 2002.

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